Add to ORKGThis report investigates an analytical evaluation of buckling modes of shell configurations to determine imperfection sensitivity of optimum structural designs for Mars entry capsule."NASA CR-1800.""June 1971."Cover title.Includes bibliographical references (p. 11-12)This report investigates an analytical evaluation of buckling modes of shell configurations to determine imperfection sensitivity of optimum structural designs for Mars entry capsule.Performed by Philco-Ford Corporation, Newport Beach, Calif. for Langley Research CenterMode of access: Internet
Various approaches to problems of delivering Apollo type entry capsule to Mars, entering and descend...
Results from a 25 shot ballistic range test of the Mars Exploration Rover (MER) aeroshell are presen...
In the field of aerospace engineering but also in the fields of civil and mechanical engineering the...
This report investigates optimum structural design for Martian entry capsule configurations ."NASA C...
Analytical evaluation of buckling modes of shell configurations to determine imperfection sensitivit...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
This report investigates optimal structural design for sandwich-shaped and ring-stiffened loaded she...
A study of the buckling of thin shells was conducted using a digital computer program for the geomet...
A FORTRAN 4 digital computer program is presented for the initial postbuckling and imperfection sens...
The modified structure method, which is based on Koiter's theory of imperfections, was used to calcu...
A study of the buckling of thin shells was conducted using a digital computer program for the geomet...
A buckling analysis and imperfection sensitivity study of scaled launch-vehicle cylindrical shells h...
Imperfections are irregularities of the shape of a thin-walled shell, such as those used for rocket ...
Guidelines dating back 50 years, NASA SP-8007, are employed today in the design of thin-walled launc...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
Various approaches to problems of delivering Apollo type entry capsule to Mars, entering and descend...
Results from a 25 shot ballistic range test of the Mars Exploration Rover (MER) aeroshell are presen...
In the field of aerospace engineering but also in the fields of civil and mechanical engineering the...
This report investigates optimum structural design for Martian entry capsule configurations ."NASA C...
Analytical evaluation of buckling modes of shell configurations to determine imperfection sensitivit...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
This report investigates optimal structural design for sandwich-shaped and ring-stiffened loaded she...
A study of the buckling of thin shells was conducted using a digital computer program for the geomet...
A FORTRAN 4 digital computer program is presented for the initial postbuckling and imperfection sens...
The modified structure method, which is based on Koiter's theory of imperfections, was used to calcu...
A study of the buckling of thin shells was conducted using a digital computer program for the geomet...
A buckling analysis and imperfection sensitivity study of scaled launch-vehicle cylindrical shells h...
Imperfections are irregularities of the shape of a thin-walled shell, such as those used for rocket ...
Guidelines dating back 50 years, NASA SP-8007, are employed today in the design of thin-walled launc...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
Various approaches to problems of delivering Apollo type entry capsule to Mars, entering and descend...
Results from a 25 shot ballistic range test of the Mars Exploration Rover (MER) aeroshell are presen...
In the field of aerospace engineering but also in the fields of civil and mechanical engineering the...